2) spinning warhead
自旋弹头
1.
At last,simulation about the three-axis warhead and spinning warhead was conducted and the results validate the feasibility of mass moment control.
5/Simulink环境下,设计开发了六自由度导弹仿真系统,并且针对三轴稳定弹头和自旋弹头进行数值仿真,仿真结果验证了质量矩控制的有效性。
2.
The varying centroid control system was studied,by which a spinning warhead realizing the terminal maneuvering.
对自旋弹头实现末端机动的变质心控制系统进行了研究。
3.
In order to express clearly and directly the relationship between controlled variables and attitude motion of a spinning warhead,the Newton dynamics method is applied to construct its attitude motion model.
为了明确直观地表现自旋弹头姿态运动与控制量之间的关系,采用牛顿力学方法建立了自旋弹头的姿态运动模型。
3) high-capacity head
高能弹头
4) High-speed Rotary Missile
高速旋转弹
1.
Research on Attitude Measurement of High-speed Rotary Missile;
高速旋转弹姿态参数测试技术研究
2.
In view of the high speed spinning and the small caliber of High-speed Rotary Missile, the small diameter non-gyro posture parameter test system is designed, and the attitude parameter of missile aviation is tested and stored.
本文针对高速旋转弹高速自旋的特点和小口径的测试要求,设计了无陀螺的小直径姿态参数测试系统,实现了弹体飞行全过程姿态参数的测试及存储。
5) high spinning projectile
高自旋弹丸
1.
A method of solving the angular speed and attitude angular of high spinning projectile was proposed by accelerometers\' specific force signal in existence of installation errors.
研究了存在安装误差时基于加速度计比力信号解算高自旋弹丸角速度和姿态角的方法。
6) high-yield warhead
高威力弹头
补充资料：自旋-自旋弛豫
自旋-自旋弛豫
磁共振成像术语。又称T2弛豫或横向弛豫(transverse relaxation)，指垂直于外磁场B0方向的磁化矢量的指数性衰减过程。磁共振成像时，对置于外磁场B0中的自旋系统施加90°射频脉冲，则自旋系统被激励，其净磁化矢量指向与外磁场B0垂直；射频脉冲终止后，被激励的质子与邻近的原子核之间发生相互作用，逐渐失去相位，净磁化矢量指向恢复与外磁场平行，该过程称自旋-自旋弛豫。自旋-自旋弛豫过程无能量交换。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条